View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 54686U 26145.61642237 +.00000000 +00000-0 +30491-3 0 00001
2 54686 97.6846 312.9123 0007002 241.1805 118.8734 15.33128717 02
| Epoch (UTC): | 25 May 2026 14:47:38 |
| Eccentricity: | 0.0007002 |
| inclination: | 97.6846° |
| perigee height: | 462 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 312.9123° |
| argument of perigee: | 241.1805° |
| revolutions per day: | 15.33128717 |
| mean anomaly at epoch: | 118.8734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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